Fuel separator and vaporizer



Dec. 29, 192- 1,56%806 F. C. MOCK FUEL SEPARATOR AND VAPORIZER Filed June 2o, 1921 5 sneetsusheet 1 Deca 29,

F. C. MOCK FUEL SEFARATGR AND VAPORIZER Filed June 20, 1921 5 Sheets-511964; 2

Dec. 29, 1925.

' 1,567,806 F. C. MOCK FUEL sEPARAToR AND vAPoRIzER Filed June 20, 1921 5 Sheets-Sheet I5 Dec. 29., 1925. y 1,567,806

l F. c. MocK f SEPARATOR AND VAPORIZER FiledJune 2o, 1921 5 sheets-sheet 4 Dec. 29, 1925- 1,567,806

F1 c. MocK FUEL SEPARATOR ANID VAPORIZER Filed June 20, 1921 5 Sheets-Sheet 5 (Ime/Dior @D mpc/ Patented Dec. Z9, i935. f

NUnire srares PATENT FRANK C. MOCK, OIF CEJCAG-O,l LLINOS, ASSIG-NOR TO STROMBERG MOTOR QE/'CES COMPANY, OF CHICAGO, ILLNIS, A COB/PCRATON F ILLINOIS.

FUEL SEPARATOR AND VAPOR'IZER.

Application filed June 20, 1921. Serial No. 478,929.

To @ZZ @0.7mm may coil/cern.' the heat to the fuel. In the developnienlJ 55 Be it known that l, l*1 remit il. Moon, a of this latter method it is first necessary that citizen of the United States, residingat the air component of the mixture should Chicago, in the county of Cook and State not be subjected to the intensified heatinif;

5 of Illinois7 have invented a certain new and along With the unvolatilized fuel: and sed# useful improvement in l `uel Sepafra'l'ms` and 0nd, that the heavy ends of the fuel should e0 Vaporizers, of which the following is a full,v remain in association with the heating clear, concise, and exact description, refeimeans for a suiicient time to vaporize thi?, once being had to the accompanying` drawsame. Inasrnuch as the average interval 1G ings, forminga part of this specification. embracing the vaporization, compression lhe present invention relates to fuel sepaand expansion of one charge at intermediate 65 rators and vapor-isere for internal coinbusengine speeds isapproximatelyl/Qth secon-.1l tion engines. it Will be apparent that the time required Owing to the continued tendency of gas/o to vaporize the heavy ends of a cha-rige is line or other liquid fuels available for the considerably longer than that available at operation of internal colnlimstion engines to this rate of operation. lonsequently it is 70 decrease in volatility, there is an urp ynt de necessary to provide means for delaying the mand for fuel treating apparatus which will passage of these heavy ends to the. cylinder conveniently and economically utilize all in order to supply suflicient heat for their E@ of the fuel by volatilizing the fuel particles vaporization. It is further desirable that of low volatility or the heavy ends of the the devices for accomplishing this end ini- 75 fuel as they are commonly called. The pose a minimum resistance to the flow of failure to volatize and burn these heavy ends the mixture to the engine, otherwise they results in a detrimental crank-case oil dilu- Will decrease the volumetric efficiency and tion and pre'inature wear in the engine beau power output of the engine.

ings in addition to the Well known starting The general theory of operation of the S0 and accelerating dilliculties and loss of related devices of the prior art is to drav:

economy. The vaporization of these heavy the .mixture into a separating chamber ends by the application of heat has been the Where it is set up in a vortex or involu'tc 3o most successful solution advanced thus far. Whirl Which throws out the heavier parln lthe manner of applying' 'this heat to the ticles of fuel by centrifugal force. These S5 heavy ends of the fuel, however, numerous heavier particles are treated according); to diilicnlties have been encountered. lt has various methods, beingusually retained in become evident from past development that Contact or being)- recirculated into Contact heat application through the medium of the With a heated surface until vaporized. The

air component of the mixture is only a mild majority of these prior constructions have 90 and inadequate method of heat application the disadvantage of heating the air compo and very detrimental. to the volumetric nent undesirably by reason of their action eniciency and power output of the engine. of circulating or moving' the air in direct ln addition to these (llisadvantai'os the higrli contact With the heating` surface or in such tenipointures that arc usually required lo relation as to receive the radiant heat there entirely vapor-izo the heavy ends in the ordifrom. These prior devices are fln'thernioi'e nary gasoline involve excessive heating' of objectionable in that they impose consi/ler'- lhe i 'n with consequent impairment of the able resistance to the flow of mixture, aus lubricating function and overlicating of the thus result in aconsiderablc reduction in engine and also cause in.ei;niitiou and de-4 lhe air flensity of the mixture ilowinfr lo 10o lerioiaion.- llt has been recognize/.ed that the engine cylinder. This disadvantage is [lic application of heat through the medium inherent in the manner in which the in' of the air component is not :i niel'l'iod of is ili'aivn from the separal'iiiu: chamber J suilicient lie-latina' intensity, (these heavy lhc engine ,fylinder. rl`he ivhirlini` motion ends frequently having boiling` temperatures to which the mixture is subjected in the in 105 sapproxiniatii i500 l?. or more) and ac volute or vortex' chamber increases the coriflingly neoourse has been had to means density-of the outer strata of mixture oivire' :for procfllg'ng `amore direct application .olf Vto the centrifugal for@ tending. t0 GXP l the mixture outwardly against the outer wall, and this obviously decreases the density of the inner strata of mixture to a rela tively low pressure. In these prior constructions the mixture is usually drawn from the center of the whirling chamber at the point where the mixture has the least density and where there is a comparatively high suction. rlhis obviously imposes vconsiderable resistance to the liow of mixture 'to the engine and materially reduces the quantity of charge obtainable by the .motor at high speeds. A further disadvantage of this practice lies in the fact that the kinetic energy which is stored up in the whirling mass of mixture is lost by the practice of drawing the charge from `the center of the vortex, this requiring the dissipation of the kinetic energy in the gas in order that it can be drawn inwardly to the central outlet port.

It is one of the fundamental objects of the present invention to provide a construction of fuel separator and vaporizer wherein the heavy ends and all unvolatilized parA ticles of fuel are separated out of the main body of air or mixture and are subjectedV to the requisite vaporizing temperature without the objectionable heating of the alf. Y

It is a further object to provide a construction wherein the supply of mixture to the engine will be drawn from the region of maximum density in the device and without loss of kinetic energy in the whirling body of mixture. This object is attained by drawing the mixture from the outer strata of the whirlingmass, either through an outlet extending substantially tangentially in the direction of whirl, or, what is its equivalent, through a lateral outlet into which the high velocity mixture Vfrom the outer strata of the whirling volume is deflected. By this arrangement a mixture charge ofl maximum density is drawn into the engine cylinders, and the velocity and kinetic energy of the whirling Abody of gas is continued into the intake manifold to the cylinders, thereby reducing the resistance to air flow to the cylinder to a negligible quantity.

A further object ofthe present invention is to. maintain anl effective separating function by causing the liquids and gases to llow laterally away from each other in opposite directions along or relative to` the walls of the whirling chamber, the liquids lbeing preferably gravitated downwardly along this wall and the gases raised upwardly under the action of the engine suction. The mixture outlet from the whirling chamber is disposed in a plane which is elevated above the plane of the inlet so thatrthere is minimum possibility of 'any of the unatomized or unvapor'ized :particles lof fuel reaching this Outlet, The gravitational discharge Of h6 fuel particles down along the chamber wall may be aided by the creation of a slight suction or circulation of a portion of the gases downwardly along this wall.

A further object of the invention is to combine with the above whirling chamber an improved construction of fuel segregating and vaporizing chamber. For the purposes of returning the gaseous products of the vaporized fuel particles from the segregating and vaporizing chamber to the mixture entering the engine, I contemplate creating a restricted circulation of a portion of the gases down into the segregating and vaporizing chamber for the purpose of p icking up the vaporized combustible products, and then recirculating these gases up into the whirling volume of mixture discharging from the device. rllhis fuel segregatjingand vaporizing chamber is thermally insulated against radiation of heat to the main bod;v of air, th'us preventing transfer of hea( lo the air either by conduction or rzuliation. Owing to the relatively low temperature at which the air is kept the vapor created in this vaporizing chamber, upon rejoining the air charge, is usually condensed into a line fog in the intake manifold, which fogr is so finely divided as to immediately vaporize again in the cylinders on the compression stroke.

The fuel segregating and vaporizing chamber functions to retain the heavy ends of the fuel in subjection to heat until theyr have become vaporized, and this as previously pointed out, involves a delay in their passage to the engine cylinders. In this regard I have provided a preliminary heating surface which has unique cooperation with the fuel segregating and vaploriz ing chamber to the end of increasing the flexibility of the motor notwithstanding the delayed passage of fuel caused by the fuel segregating and vaporizing chamber. This preliminary heating surface is preferably in the nature of a hot spot positioned to receive the impinging particles of fuel as they enter the present device from the carbureter. This hot spot is preferably limited in area in order that it will vaporixe only the more volatile particles oi" fuel. for the reason that if this hot spot were made, sufficiently large to volatilize the heavy ends and all of the fuel particles, it would produce the undesirable heating of the air previously referred to. It will thus be seen that this preliminary hot spot and the segregating and vaporizing chamber cooperate by the action of the preliminary hot spot vaporizing the more volatile particles of fuel and the vaporizing chamber vaporiaing the less volatile particles of fuel which must be retained in delayed contact with a heating surface. During periods of accelera tionparticularly when the device is aswei/nec sociatcd with a carburetor having an accelerating well or other temporary fuel enriching means, the quantity of these unvolatilized fuel particles is increased. The correlation between the preliminary hot spot and the vaporizing chamber increases the flexibility ot' the motor during these periods by virtue ot the preliminary. hot spot vaporizing the unvolatilized` particles of this increased charge and maintaining' the temporary richness of the mixture over the period oli delay incident in the vaporizing action ol'" the vaporizing chamber.

Other more specific objects and advantages will hereinafter appear. @ne general embodiment of the invention is illustrated in the accompanying drawings in which:

Figure l is a fragmentary elevational view oi an internal combustion motor illustrating my `device applied thereto;

Figure is an. enlarged vertical sectional view through the fuel separator and volatilizer; p

Figure 3 is a horizontal sectional View talren on the plane ott the line of Figure 2;

iiigure el is a similar sectional view talren on the plane ot the line lf-ft ot TEigure 2;

Figure da is a fragmentary view illustrating the fuel guiding plate;

Figure 5 is fragmentary vertical s ectional View taken on the plane oli the line 5---5 of Figure lg Figure 6 is a view similar tolligure 2, illustrating a modified form;

Figure 7 is a horizontal sectional view taken on the plane oi the line 7-7 ot Figure G; l

Figure S is a vertical sectional view ot another modified torni;

1Eigure 9 is a horizontal sectional view thereof talren on the plane ot the line 2)9; and v Q L Figure lO is a vertical sectional view oi. still another -foi-m oli the device.

Jtetei'ring to Figure l, the present i'uel separating and volatiliaii'ig device, which is designated l in its entirety, is supported iointly by the intake maniiold ll and an exhaust conduit l2 receiving the exhaust ga es ii'oni the exhaust nianilold i3, A. suitable design ot carburetor lil (preieiably haring a horizontal outlet) may be mounted onV the e'lev'ice l0 lo deliver nurture tl'iereto. The outlet liroin the l'uel separating and vapori 'nu' device has direct con uection with the intuire manifold ll. .lllie bottom portion ol. the device l0 has eonneclion in the exhaust conduit .lil for the ilow o' exhaust gases therethrough in proximity to the vaporizing cl'iainber, the conigections lfor this exhaust circulation beine arranged as indicated i'or the circulation ot the entire volume oi the exhaust gases; or being au ranged in shunt ci the exhaust conduit er in a similar relation thereto whereby the volume et exhaust gases flowing through the separating and vaporizing device can be readily controlled.

The combined fuel separating and volatilizing chamber is built up of lower, intermediate and upper horizontal sections 15516 and l?, respectively, which are connected together by a bolt 18 extending through the several sections and project ing from the bottom of the lower section l to receive a nut 19. The lower section l5 is constructed Vas a bowl shaped casting consisting of a cylindrical wall 2l and a curved bottom 22. This casting is formed with diametrically opposite inlet and outlet connections 23 and 2a for connection in the exhaust conduit l2; the sectional view of Figure 2 looking at the device from the opposite side from that viewed in Fig. l, which accounts for the apparently reversed circulation of the exhaust gases through the connections 23 and 24. The upper edge oit' the wall 2l is formed with a peripheral flange 25 adapted to cooperate with a similar flange 2G on the lower edge of the intermediate section lf",l ears 28 on these flan s being adapted to receive cap screws or bolts for joining the two sections together. Clamped between the opposing ilanges 25 and 26 is the marginal flange 29 of a cylindrical sheet metal shell 3l, preferably constructed of brass or copper. rlhe curved bottom 32 of this shell, which is formed with concentric corrugations 33 for increasing the effective heating area thereoi constitutes the top of the circular exhaust gas chamber Bel and the bottom of the cir cular fuel vaporizing chamber The center of the corrugated bottom 32 is apen tured to receive the tubular clamping nut 36 which threads down into a boss Bi and closes the bottom of this sli-eet met shell against leakage around the tie bolt i8. lt will be noted that this mounting of the shell 3l permits of its convenient removal for cleaning or substitution. ln addition to increasing the ellective heating area of the vapoiizing chamber 35, the corrugations 33 constitute a series olf separate pockets for receiving and distributing` the entinincd particles of fuel iuiiliorxnly orer the ouH tire heating suri'acc, it beii noted that 'the relatively thin section oil this heating surface will result iu the quick and intense heat ing oit the uel accuinmulating thereon, lille top of the vaporiaing chainl'ier 35 is delned by a circular dish 3% which is mounted ou 'the tie bolt 1S through a hub 39 pinned thereto. The edge oi" the dish is spaced :troni the interior wall of the shell. 3l to provide the annular opening il., and adjacent its center this disk is provided with a plurality ol openings 4t2, for a purpose which l shall presently describe, This dislr or shield is preferably constructed of successive laminations of metal 40 and asbestos or other heat insulating material for minimizing the amount of heat radiated up into -the separating chamber. f

The intermediate easing section 16 consists of a cylindrical wall 43 formed at one side with a tangential or involute intake passageway 44. This intake vpassageway is flanged as indicated at 45 to receive the conventional flange 46 on the mixture outlet of the carbureter. The intake passageway 44 may, if desired, be formed with aconstricted discharge opening 47 for accelerating the velocity of the mixture as it enters the device. A relatively small hot spot 48 is formed on the outer-wall of the inlet passageway 44 in proximity to the 'discharge opening 47, in proper position for receiving the impinging particles of unatomized fuel entering the inlet passageway from the carbureter. Where the constricted outlet 47 is formed in this passageway, the mixture, and particularly the heavier fuel f particles, are crowded over against the hot spot 48 for vaporization of these fuel particles. The spot 48 is heated by a branch conduit 49, which, as shown in Fig. 5, extends upwardlyv from the exhaust gas chamber 34.

During certain operating conditions there is a tendency for a considerable quantity of the fuel to enter the inlet passageway 44 in liquid condition, which fuel enters the separating chamber 52-53 by running along the walls-of the inlet passageway and discharging from the edges or shoulders 50 at the intersection of t-he inlet passageway and separating chamber. The globules of liquid fuel have a tendency to tear or whip off these shoulders into the air stream, particularly from the upper or inclined shoulders from which a dripaction can occur. This action is undesirable for there is the possibility of these large globules of fuel being drawn into the engine by the air stream. l-Xccordingly, I have provided an inclined lip 51 (Figure 4) which extends diagonally down from the highest point of the throat outlet 47 into coincidence with the circular wall of the separating chamber in order to guide the streamfof liquid fuel down upon the walls of the chamber without allowing it to be whipped off into the air stream. Thisdiagonal lip maybe cast integral at the throat outlet 47 or it may constitute part of a plate 51 which is suitably fastened to the circular wall of the separating chamber as shown. This guiding lip is preferably arranged to form Ia channel directly in its rear to receive and guide onto the walls of the separating chamber any stream of fuel flowing along the inner or bottoni walls of the inlet pas- Segway 44;.:

The upper part 5B of the whirling` chamber is defined in the upper casing section 17 which is flanged as indicated at 54 to 'be secured to the upper flange 55 on the intermediate casing section 16, these two flanges being provided with matching lugs 28 for the reception of cap screws or the like, and having an interposed gasket 5G for sealing the joint. This upper casing section consists of a central web 57 and a peripheral channel portion 5S of inverted U-shaped cross section which is open at the bottom and which rises in vertical dimension as it progresses towards the tangential mixture outlet 59. portions 53 and 52 of the whirling chamber are connected through an annular passageway 61 defined between inner and outer sheet metal shells 62 and G3. The inner shell 62 is secured by rivets G4 to the casing web 57 and is tapered inwardly at its center to snugly embrace the tie bolt 1S. The outer shell G3 has a central inlet opening 65 at its lower end, and at its upper end is formed with a horizontal flange G6, forming part of the floor of the chamber portion 53, and is also formed with a vertical flange 67 by which the shell is suitably secured to the casing 16-17. The outer edge of the shell 62 is saaced from the flanged portion 66 to form t 1e curved outlet 68. T his outlet is tapered down to a reduced throat portion which opens into the bottom of the chamber portion 53 throughout substantially the entire circumference of the chamber. The channeled chamber portion increases in width as well as in height progressively towards the mixture outlet 69 so that the resulting chamber or passageway is of tapering form rising in a helical curve towards the tangential mixture outlet 59. This outlet is flanged as indicated at 69 for connecting with the conventional manifold flange.

As the mixture enters the device through the intake passageway 44 the inertia of the heavier, unatomized particles of fuel results in their impingement against the hot spot 48, so that these fuel particles will be sub- `iected to a brief vaporizing action immediately upon egress from the carlnirctcr. but without involvilig undue heating of the air. The lighter, more volatile particlesI of fuel are vaporized on this hot spot and pass oil' into the mixture for immediate co11\.'e vame to the engine cylinders, while the heavier ends pass into the separatiilg chamber 52- 53 where they are separated out on the walls of the chamber for precipitation into the fuel segregating and vaporizing chamber 135. The carbureter 14 will he presumed to have an accelerating well or some other equivalent fuel enriching device forv acceleration. and it should be noted that during this period the quantity of unvolatilized fuel is increased with the increased richness of mix- The upper and lower lll() ture. At this time it is desirable that the increased richness of mixture or a considerable proportion thereof be immediately conveyed to the engine to obtain the desired responsiveness and it will be noted that to this end the hot spot 48 immediately vaporiZes a considerable proportion of the unvolatilized particles of the increased charge for direct conveyance in the mixture stream. This hot spot also tends to prevent the drop in temperature which usually occurs with the sudden discharge of the contents of the accelerating well into the mixture stream.

The mixture entering the whirling chamber tangentially produces a high velocity vortex motion which. throws the heavier fuel particles out into contact with the walls a3, from whence the accumulation of fuel drains downwardly into the vaporizing chamber 35. The air with its volatilized fuel is then drawn inwardly to the opening 65, the mixture still retaining its whirling or involute motion. This motion continues up through the annular passageway (31 and into the rchamber area 53, from whence the whirling mixture is drawn off tangentially through the outlet passageway 59. The upper chamber area 53 is illustrated as being of the same diameter as the lower `chamber area 52 for compactness of form and simplicity of construction, although it is to be understood that this upper chamber area may be extended to a greater diameter if desired for increasing the centrifugal effect therein. This also applies to the other forms to be later described. In the construction illustrated the contraction of the whirling Vortex occurring in the annular passageway 6l constitutes a balanced point in the contained body of mixture for the reason that the outwardly expanding centrifugal force occurring above this passageway substantially balances the retarding effect tending to restrain the inward contraction of the vortex below the passageway. As above intimated, however, by proportioning the respective diameters of the upper and lower chamber areas 53 and 52 dilferent'efiects may be obtained. ,lhe kinetic energy created in the whirling volume of mixture is retained up into the upper chamber area 53 and out into the intake manifold by reason of the tangential arrangement of the outlet passageway 59, and obviously this outlet draws mixture from a point of maximum density in the device. The ascension of the mixture intov the intermediate passageway 6l creates an upward draft through the openings 42 and the expansion of the mixture alongl the walls 43 produces a limited downward circulation of mixture into the vaporizing chamber. These together create a circulation of a limited volume of the mixture down through the annular opening il and through the vaporizing chamber 35 and upwardly through the openings e2, to join the ascending body of mixture. The annular film of mixture circulating downwardly through the opening di stinnilates the descent of the particles of liquid fuel. on the walls i-3 and 3l into the vaporizing chamber 35, and this limited volume of mixture in flowing through the chamber 35 and up through the holes 4t2 picks up the gasilied fuel created in the vaporizing chamber and unites the same with the main volume of mixture ascending through the passageway 6l.

As an alternative construction, the intermediate passageway 61 with its openings 65 and 68 may be eliminated as shown in Figures G and 7. In this arrangement, the outer strata of mixture remains in contact with the outer walls of the whirling chamber and rises into the helical portion 53 without undergoing any contraction of the vortex. The tangential outlet 59 receives the outer strata of mixture of maximum density directly from the chamber portion 53, and, as before, the kinetic energy created in the vortex of mixture is retained into the intake manifold. As in the previous enibodi* ment, the volatilized constituents of the mixture are separted from the heavier particles of fuel by a lateral separation occu ring on the walls 43, the volatilized fuel ascending with the air up into the chamber portion 53 and the heavier fuel particles descending under a gravitational discharge down into the vaporizing chamber 35.

As shown in Figures 8 and 9, a tangential discharge -of the mixture may be obtained by deflecting the mixture out of the chamber by vanes or the like, which project into a region of maximum density and avoid loss of kinetic energy. As shown in the latter form, the outlet discharge occurs through an outlet conduit 72. This discharge conduit is flared outwardly at its lower end as indicated at 73, where it is formed with a flange 74, adapted for boltA ing to the upper flange of the interM mediate casing section. A circular plate or disk is spaced from the bell shaped portion 78 to provide an annular passageway 76 therebetween, this plate having a plurality of vanes 77 formed around its circumference on the under side thereof. A shell 70 contracts the vortex of mixture and guides the same outwardly into the vanes 77, the shell 70 closely fitting the bottoms of the vanes. As shown in Figure 9, the leading edges 78 of these vanes extend v forwardly against the motion of the mixture so as to throw the intercepted mixture outwardly into the plane of the annular passageway 76. If desired the outer ends of these vanes may also be scooped with their lower edges extending forwardly so as to lll) throw the mixture upwardly through the annular passageway 7G under its own kinetic energy. In the operation of this embodiment the separation of the unvolatilized particles is eh'ected as before described, and thereafter the whirling mixture upon encountering the vanes 77 is thrown outwardly and upwardly with sufficient inertia to discharge the mixture through the passageway 76 without loss of density or kinetic energy.

In the modilied form shown in Figure l0 the mixture flowing into the separating chamber through the tangential inlet 44, past the hot spot 48, enters a helical channel 8O which spirals downwardly l'roin the inlet passageway, as indicated in dotted lines. The inner side oiE this channel area 8O is defined by a cylindrical shell 8l which is flanged at 82 'for supportbetween the flanges 83 83 on the casing sections 84. and VS5. rlhe lower edge of the shell 81 is preferably formed with an outward slope 86 which serves to deliect the liquid fuel accumulating on the shell down into the vaporizing chamber 35 in a particular manner which I shall presently describe.

As I previously emphasized, it is very desirable to avoid undue heating of the air, but at the same time a high temperature in the vaporizng Chamber is essential to the effective vaporization of the heavy ends of the fuel. The relatively thin, sheet metal bottom 32 of the vaporizing chamber may attain a luminous temperature with consequent rapid heat transfer by radiation and conduction. As before described, the shield or disk 38 of asbestos and metal minimizes the radiation of heat to the main body of air. The walls of the separating chamber tend to become quite hot by direct heat conduction from the vaporizing surlace 52. To minimize the heating of the air resulting from contact with lthese walls the channel and the shell.

there is provided a sheet metal Ishell 87 in in'nnediate spaced relation to the outer walls of the channel area, this shell maintaining a film oi air or mixture between the walls of The mixture en ters through aligned openings in the channel wall and in the-shell, the opening in the shell being indicated at 88, and thence revolves around in contact with the inner wall ot the shell 87 to avoid contact with the walls ot the casing section 84;. The shell 87 is suspended by an upper flange 89 which is suitably secured to the upper wall ot' the channel SO, the lower edge of the shell projecting down below the lowest point to which the main body of air descends and hanging free to prevent heat conduction thereto.

Due to the turbulence of varying air currents existing in the mixture stream there are occasioned splashing drops which do not follow the law ol? centrifugal action but get on the inner side rather than on the outer side ot the mixture passages and tend thence to be carried up to the motor. I have found that in addition to the use ol centrifugal iorce it is necessary to provide means whereby these drops will be drawn. oli' or led off into the vaporizing chamber, similarly to the action ot the inclined lip 5l, and the idea and manner of drawing f off these extra drops is quite an in'iportant part of the invention. Many variations in construction are possible but they all coinprehend the use ot an edge, wire, surlacc, groove or equivalent arrangement for guiding these drops into the vaporizing chainber. In Figure l() there is shown the. use oil spirally inclined wires Si() secured to the slope 8G tor guiding the drops into the vaporizing chamber.

The corrugated bottom ol the vaporiZing chamber is depressed centrally as indicated at 92 to counteract the tendency ot the liquid fuel to pyramid at this point. The mixture whirling upwardly through the cylindrical shell 8l expands outwardly into the upper chamber area 93 which is of: substantially the same radius as the lower channel area 80. From this point the vortex oic mixture is discharged through the usual tangential out-let 59 previously described.

It will be obvious that various changes may be made in the general embodiment hereinbeiore described without departing from the essence ot' the invention` as set forth in the appended claims. y

I clailn:

l. In combination, a circular separating chamber adapted to circulate a gas for an internal combustion engine, a substantially tangential inlet passageway entering sai-d chamber, a substantially tangential outlet passagemiy leading from said chamber, said passageways producing a 'whirling vortex of the gas in said chamber to ell'ect thc separating function, and means l'or preventing the discharge through said outlet passageway of the constituents separated from said gas.

2. In combination, a circular separating chamber adapted to receive a gas for an internal combustion engine, a substantially' tangential inlet passageway opening int-o said chamber, the circulation ot gas through said chamber creating a whirling vortex therein, an outlet passageway leading ironi said chamber at a point adjacent the pcriphery of said whirling vortex, said outlet passageway being displaced axially to one side of said inlet passageway, :india chamber to the other sideI ol said inlet liiassageway for receiving the constituents separated from said gas.

il. In combination, a substantially verti- 'cal fuel separating and vaporizing chamber,

a substantially tangential inlet passageway leading;` thereto, an outlet passageway leading from said chamber yaxially above said inlet passageway, said passageways imparting a whirling motion to the mixture in said chamber, and a fuel vaporizing surface in the lower end of said chamber ren'ioved from the region of the whirling volume of mixture.

i, In combination, a. fuel separating and i-*aporizing chamber, a substantially tangential. inlet passageway opening into said chamber and imparting a whirling motion to the mixturr-.i therein, an outlet passageway leai'liiig from said chamber above id ii'ilet pas; sway, a fuel vaporixiiig surface in the end of said chamber below said inlet passageway, means for heating said surface, and a baliie member interposed between the whirling volume of mixture and said vaporizing surface, said baile permitting the precipitation of fuel particles to said Vaporizing surface along the walls of said chamber.

5. ln combination, a substantially vertical fuel separating and vaporizing chainber, a substantially tangential inlet passageway opening into said clian'iber and creating a whirling vortex of mixture therein, an outlet passageway leading from said chamber above said inlet passageway and at a point adjacent the periphery of said whirling vortex, a fuel vaporizing surface in the bottom of said chamber, and a baffle spaced from the walls of said chamber and interposed between the region of said whirling vortex and said fuel vaporizing surface. 1

6. In combination, a substantially vertical cylindrical fuel separating chamber, a substantially tangential inlet passageway entering said chamber and creating a whirling vortex of the mixture therein, an outlet passageway leading from said chamber above said inlet passageway and at a point adj acent the periphery of said whirling vortex, a corrugated vaporizing surface in the bottom of said chamber, means for circulating exhaust gases below said corrugated surface, and a disk supported above said vapoi'izing surface and having apertures therein adapted to induce a restricted circulation of mixture down into proximity to said vaporizing surface.

7. The combination with a mixture passageway extending from a carburetor to an internal combustion engine, of a fuel separating chamber interposed in said mixture passageway, a first heating means in said mixture passageway for vaporiziiig 'the more volatile particles of fuel, and a second heating means comprising a centrifugal separating chamber cooperating therewith for vaporizing the less volatile particles of fuel.

`8. ln combination, a mixture pass extending from the carhurcter to ternal combustion engine, a fuel sep chamber constituting a part of sai ni passageway, a first heating surface so t posed in said passageway as to receive fuel particles separated. by velocity impin ment on said first heating surface, a centrifugal separating chanilicr posterior to said first heating surface, and a second heating surface cooperating therewith for heating the fuel particles which hare been separated out of the main body of mixture by said centrifugal separating chamber. u

l). ln fombination, i .('zzubureter hari.

means for enriching the mixture upon :iccelcration, a mixture passageway cxlieiniiing from said carburetor to the internal conibustion engine, a fuel separating chamber constituting' part of said mixture passageway, al first heating surface in said passageway for heating fuel particles iii their travel into said fuel separating chamber and a second heating surface cooperating therewith and removed from the path of the main body of mixture for heating the fuel particles separated therefrom, said first heating surface operating to volatilize a sufficient proportion of the fuel in the accelerating' charge to insure prompt accelerating response of the engine.

l0. A` mixture passageway adapted to extend from a cai'bureter to an inteinal coinbustion engine, a fuel separating chamber constituting a part of said mixture passageway, a first heating surface in said passageway substantially in line with the intake opening of said passageway and anterior to said fuel separating chamber, the main volume of mixture flowing in contact with said lirst heating surface, and a second heating surface in said passageway, said second heating surface being removed from Contact with the main volume of mixture and operating to vaporize the fuel particles separated therefrom.

ll. In combination, a mixture passageway adapted for circulating the mixture for an internal combustion engine, a fuel separating chamber constituting part of said passageway, a vaporizing surface for vaporizing the fuel particles separated out of the mixture in said chamber, and a heat insulating baffle for preventing the main Volume of mixture from contacting with said vaporizing surface. i

12. In a device of the class described, the combination of a centrifugal fuel separating chamber, a Vaporizing surface for receiving the separated particles of fuel, and means for thermally insulating the fuel mixture in said separating chamber against heat from said vaporizing surface thereby preventing undue heating of the air in the mixture.

13. In a device of the class described, the

combination of a centrifugal fuel separating chamber, a vaporizing surface for receiving the fuel particles, a surface upon Which the fuel particles tend to accumulate, the fuel particles on said latter surface being susceptible to being Whipped off into the mixture stream, and means adapted to counteract this tendency by guiding the fuel particles from said latter| surface out of the path of said mixture stream.

14. In a device of the class described, the combination of a fuel separating chamber, a vaporizing chamber for receivingthe fuel particles separated from the main volume of mixture, a surface tending' to receive accumulations of liquid fuel, the fuel thereon being susceptible to being Whipped into the mixture stream, and diagonal guide means operatingl to counteract this tendency by guiding the particles of liquid fuel from said surface to said vaporizing chamber.

l5. In a device of the class described, the combination of a fuel separatincr chamber comprising outer and inner spaced utils, a fuel vaporizing chamber, one of said walls dischargingr the fuel accumulatingr thereon directly into said vaporizing` chamber, the other of said Walls terminating at a point removed from said vaporizinp chamber, and fuel guiding means depending from the edges of said latter Wall for conductingr the fuel accumulatiner on said Wall into 4said vaporizing chamber.

In Witness whereof, I hereunto subscribe my name this 31st day of May, 1921.

FRANK C. MOCK. 

